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WO/2023/192087A1 |
A drone with extendable and rotatable wings and a multiple accessory securing panel is provided. The extendable wings help increase the lift of the drone and reduce the air drag on the drone. The multiple accessory securing panel allows ...
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WO/2023/180381A1 |
The present invention relates to an electrically driven ducted fan engine (10), comprising a housing (12) with an inner housing wall (12a), defining a substantially cylindrical inner space (14) and a longitudinal axis (L), an inlet openi...
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WO/2023/177774A1 |
A vehicle for travelling on a road and in the air is provided, comprising a fuselage extending from a forward to a rear end along a horizontal longitudinal roll axis, a pair of main wings mounted on the rear end of the fuselage, a pair o...
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WO/2023/172357A2 |
Aircraft (20) and airfoils (24) for more efficient flight operations using electric motors. An aircraft (20) includes an airfoil (24) and a thrust device (44) rotatably mounted within the airfoil (24). An airfoil (24) includes a top surf...
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WO/2023/167130A1 |
[Problem] To improve the flight performance of an aircraft. [Solution] This aircraft on which a passenger can ride, and which moves by floating from the ground, is characterized by comprising: a fuselage on which the passenger rides; lif...
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WO/2022/204239A9 |
A flight control arrangement for a hybrid aircraft includes a fixed-wing flight (F/W) control module and vertical takeoff/landing flight (VTOL) control module. The F/W control module is an integrated component having a respective network...
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WO/2023/157189A1 |
This aircraft performs vertical takeoff and landing. The aircraft is provided with: at least a pair of fixed blades 20-j; a rotor blade 402-1 that is rotary driven to generate a propulsion force for propelling the aircraft vertically upw...
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WO/2023/155498A1 |
A self-charging tail-sitter unmanned aerial vehicle adapted to a launcher. The structure of the unmanned aerial vehicle comprises: a head propeller (1), a propeller driving motor (2), foldable wings (6), a wing actuating motor (5), a fus...
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WO/2023/152746A1 |
An aircraft, comprising: a fuselage; two wings mounted to the sides of the fuselage, extending laterally; a pusher propeller, statically mounted to the fuselage, wherein a rotational axis of the pusher propeller is parallel to a longitud...
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WO/2023/136815A1 |
An electric vertical take-off and landing vehicle includes a fuselage containing an internal compartment which may be used to transport a person, animal, or object. The fuselage includes a canard located at a forward portion of the fusel...
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WO/2023/136918A1 |
A system for establishing a primary function display for an electrical vertical takeoff and landing aircraft. The system further includes a plurality of sensors that detects at least a metric and generates at least a datum based on the a...
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WO/2023/132478A1 |
According to an embodiment of the present invention, provided are a vertical takeoff and landing aircraft using a hybrid propulsion system and a control method therefor, the aircraft comprising: a thrust propeller (81) for generating thr...
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WO/2023/123682A1 |
The present invention provides an aircraft having a double-row wheel counter-rotating pneumatic effect, comprising a wing plate, rotating assemblies, and a landing gear, wherein the wing plate is connected to a position directly above ea...
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WO/2023/126701A1 |
A method for estimating rotor torques (TQmast1, TQmast2,…,TQmastN) of an aircraft (1; 1'; 1'') capable of hovering and comprising a plurality of rotors (31, 32; 33', 34'), which are rotatable under the action of respective rotor torque...
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WO/2023/128962A1 |
The present invention relates to an aircraft capable of vertical landing-takeoff, which has arms with folding mechanisms and safety systems that minimize the risks that may occur during an accident, and its feature. The vehicle chassis (...
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WO/2023/129444A1 |
Aspects relate to a system for flight plan generation of an electric vertical takeoff and landing (eVTOL) aircraft. An exemplary system for flight plan generation includes a flight controller mounted on an eVTOL aircraft. The flight cont...
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WO/2023/126919A1 |
A VTOL-type air vehicle is transitioned from forward speed mode to hover mode via a transient path in transition mode. The air vehicle includes first and second propulsion systems, and high lift, mild stall fixed wings. The first propuls...
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WO/2023/122717A1 |
A method of operating an aircraft including takeoff of an aircraft; transitioning the aircraft to a forward flight configuration by increasing an amount of forward propulsive force generated by a propeller assembly from equal to or less ...
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WO/2023/121784A2 |
A tiltrotor aircraft comprising a wing carrying an engine on each wing half, and a fuselage-mounted third engine with a transmission system configured to drive each of the tilting rotors from the third engine. The engines may be any powe...
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WO/2023/121436A1 |
Vertical take-off and landing (VTOL) aircraft of the fixed-wing type, comprising a centre section defining a centreline of the aircraft, and a pair of wings, arranged on either side of the centre section, wherein the wings extend longitu...
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WO/2023/122109A1 |
An aircraft has port side and starboard side propeller blades that each have a portion of the blade hidden or overlapping with the fuselage. This hidden or overlapping blade may extend into a slot of the fuselage. The advancing or retrea...
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WO/2023/113908A1 |
An unmanned aerial vehicle (UAV) includes lift rotors and control rotors. The lift rotors are mounted to the UAV and oriented to provide a first vertical thrust to the UAV. The control rotors are mounted to the UAV outboard of the lift r...
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WO/2023/100150A1 |
A control unit (46, 46') for an aircraft (1, 1') capable of hovering or for a flight simulation system of the aircraft (1, 1') is described; the control unit (46, 46') is programmed to: - receive in input a plurality of data associated w...
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WO/2023/092183A1 |
Embodiments relate generally to systems and VTOL aerial vehicles. An example central server system comprises: at least one central server system processor; and central server system memory storing central server system program instructio...
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WO/2023/084138A1 |
The invention relates to a manned or unmanned jet-propelled aerial vehicle, made up of a housing (1) containing at least one engine (2), such that the housing (1) has a suction opening (3) at the bottom, where the engine (2) is located, ...
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WO/2023/079433A1 |
The present invention relates to a vertical take-off and landing module (200) for a fixed-wing aircraft (110), which includes at least one vertically-acting propulsion unit (240), actuator means (245) and support means (230), so as to be...
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WO/2023/059209A9 |
The method of obtaining both, lifting force and thrust, required for horizontal flight of the vertical take-off and landing flying machine while maintaining horizontal flight stability of the machine which is realized due to suction atmo...
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WO/2023/079964A1 |
This flight control device performs flight control processing for causing an eVTOL to fly. The flight control device sets an operating mode to one of a plurality of failsafe modes in accordance with which of a plurality of normal modes t...
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WO/2023/081387A1 |
A rotary wing vehicle has a vehicle body. A gimbal assembly mounted to or within the body. A propeller assembly is mounted to the gimbal. The propeller assembly has first and second fixed pitch propellers. The gimbal assembly has a first...
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WO/2023/067432A1 |
Systems and methods for an aircraft comprising: wings in tandem configuration wherein each wing having one tilting motor; an additional tilting motor located at the rear part of said aircraft; wherein all said tilting motors can tilt in ...
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WO/2023/067253A1 |
The invention relates to a flying device comprising a main body, to which a combustion engine (MC), an electric motor (ME), an electricity generator (GE) and an electrical energy transfer circuit (300) are attached. The combustion engine...
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WO/2023/067339A1 |
A VTOL aerial vehicle (10) is disclosed, comprising: an airframe (12); one or more arms (202) coupled to the airframe (12) at a pivot (206); and three or more propulsion units, each mounted on a gimbal (16) having a gimbal axis, and each...
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WO/2023/067252A1 |
The invention relates to a method (100) for correcting the thrust vector created by a thrust assembly associated with electrical means for correcting said thrust vector. Such a thrust assembly comprises a mechanical rotor rotated by a ro...
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WO/2023/062514A1 |
A vertical take-off and landing (VTOL) vehicle (1) has a main body (10) including airfoil sections (13) on either side of a central module (20) in which a load may be carried. Articulated forward thrust systems (SOL, 50R) are mounted on ...
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WO/2023/051013A1 |
The present patent discloses a vertical take-off and landing aircraft based on variable propeller wing technology and a double-propeller wing layout. A main wing surface employs a propeller wing design and may be switched between a rotor...
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WO/2023/056093A1 |
Systems, methods, and apparatuses for an aerial vehicle (AV). The AV can include a frame structure comprising an upper frame, a lower frame, and bridges connecting the upper frame and the lower frame. The upper frame can include a housin...
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WO/2023/051929A1 |
The invention relates to an aircraft, comprising: at least one pair of wings (2, 3) for an aerodynamic flight; a flight propulsion drive (10) acting mainly in the forward direction (u) for the purpose of said aerodynamic flight; and a ho...
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WO/2023/048779A1 |
Vertical take-off/landing and horizontal straight flight aircraft for transportation of passengers, cargo, and/or goods are described herein. The aircraft have increased thrust and flight speed; improved controllability and maneuverabili...
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WO/2023/049497A1 |
The disclosure relates to a transitional aircraft. Specifically, the disclosure relates to a transitional aerial vehicle (AV), having a closed polygonal wing member allowing for, inter-alia; smaller dimensions (footprint) compared to AV ...
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WO/2023/046632A1 |
In a Ducted fan engine (1), configured for providing thrust for an aircraft (too), in particular an aircraft (100) having vertical takeoff and landing capability, comprising a fan stator (3) having one or more substantially radially exte...
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WO/2023/044011A1 |
A mobile drone communication and control system comprises a mobile drone station configured to be driven to a work area; a scanning drone carried by the mobile station and configured to scan an image of the work area and transmit the sca...
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WO/2023/044007A1 |
A drone communication and control system which utilized a mobile drone station which has capabilities of fueling hydrogen or liquid hydrogen drone, a communication control unit between the drone and the mobile drone station, a communicat...
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WO/2023/037014A1 |
Described is an aircraft, in particular a drone, having a supporting body (2) and at least two propulsion assemblies (4, 8), which are arranged on the supporting body (2) spaced apart from one another and which are designed to generate a...
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WO/2023/038684A1 |
The present disclosure describes autonomous flight safety systems (AFSSs) that incorporate an autonomous flight termination unit (AFTU) enabling AFSS monitoring for various termination conditions that are used to activate a flight termin...
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WO/2023/039066A1 |
A system which includes a plurality of cylindrical battery cells that have a uniform orientation, where each of the plurality of cylindrical battery cells has a first planar surface and a second planar surface. There is also a thermal ma...
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WO/2023/033662A1 |
The airplane has at least one fuselage (1) and at least one dorsal stringer (6) located parallel to the longitudinal axis of the fuselage (1), and each of the dorsal stringers (6) is rigidly fastened to the fuselage (1), while the center...
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WO/2023/023828A1 |
The present invention relates to an innovative type of electric and/or hybrid digital glider drone with a steerable balloon for personal flight. The project consists of a compact ellipsoidal balloon with a self-levelling drone with rigid...
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WO/2023/027612A1 |
The inventions relate to the field of aviation. An aircraft comprises a multisided body having rotatable cylinders (1) mounted about the perimeter thereof. For supplying air into the aircraft, the body is provided with inlets (2) that le...
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WO/2023/027611A1 |
The invention relates to the design of unmanned vertical takeoff and landing aircraft. The claimed device comprises a multisided body having rotatable cylinders (1) mounted about the perimeter thereof. Situated inside the body is a gas i...
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WO/2023/021099A1 |
A system for controlling yaw during vertical take-off and landing (VTOL) operation of an airborne craft, where the airborne craft comprises multiple crossflow fan lift, propulsion and control elements (LPCEs) disposed around a central lo...
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